Electrically actuated aircraft brakes

Details Electrically actuated aircraft brakes Electrically actuated aircraft brakes

F - Mech Eng,Light,Heat,Weapons

16

D

F16D 66/02 (2006.01) B60T 13/74 (2006.01) F16D 55/00 (2006.01) F16D 65/14 (2006.01) F16D 66/00 (2006.01)

Patent

CA 2588520

An electrically actuated aircraft brake with a carbon-carbon composite heat pack (10, 12) and an electrical actuator (14) for engaging the heat pack and operating the brake. When the brake is not being applied, the brake actuator is adjusted in dependence upon temperature, for example, by controlling the actuator to maintain a temperature regulated position.

L'invention concerne un frein d'avion commandé de manière électrique au moyen d'un dispositif thermique (10, 12) et d'un dispositif (14) de commande électrique destiné à venir en contact avec le dispositif thermique et à commander le frein. Lorsque le frein n'est pas utilisé, le dispositif de commande de frein est réglé en fonction de la température, par exemple, par réglage du dispositif de commande, de façon à maintenir une position régulée par la température.

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